Factors Affecting Transition Reynolds Numbers on Models in Supersonic Wind Tunnels
- 1 July 1954
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 21 (7) , 497-498
- https://doi.org/10.2514/8.3095
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Variation of Transition Reynolds Number with Mach NumberJournal of the Aeronautical Sciences, 1953
- Turbulence in Supersonic FlowJournal of the Aeronautical Sciences, 1953
- Aspects of the turbulence problemZeitschrift für angewandte Mathematik und Physik, 1952